# Service difficulty reports: N76752, cancelled Sep 25, 2006 A list on [N76752, cancelled Sep 25, 2006](https://openairdocs.org/deregistered/N76752-2006-09-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 97 reports - [SDR XN0A1329](https://openairdocs.org/sdr/XN0A1329.md): Start Valve · malfunctioned · May 12, 2006 · N76752 · Boeing 727227 · Engine Start Valves/Controls > ON PUSHBACK AT PHL COULD NOT GET NR 1 START VALVE TO OPEN ELECTRICALLY. COULD NOT DUPLICATE, OPERATED NR 1 START VALVE NUMEROUS TIMES, SYSTEM OPS CHECK GOOD IAW B727 MM CHAPTER 80-11-11. DMI 6492 CLEARED. - [SDR XN0A1320](https://openairdocs.org/sdr/XN0A1320.md): Brake Assy · dragging · Apr 20, 2006 · N76752 · Boeing 727227 · Landing Gear Brake System > ON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR 1 MLG WHEEL ASSY IAW B727 MM CHAPTER 32-45-01, OPS CHECKS AND LEAKS GOOD. - [SDR XN0A1920](https://openairdocs.org/sdr/XN0A1920.md): Brake Assy · dragging · Apr 20, 2006 · N76752 · Boeing 727227 · Landing Gear Brake System > ON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR 1 MLG WHEEL ASSY IAW B727 MM CHAPTER 32-45-01, OPS CHECKS AND LEAKS GOOD. - [SDR XN0A1284](https://openairdocs.org/sdr/XN0A1284.md): Switch · inoperative · Dec 14, 2005 · N76752 · Boeing 727227 · Leading Edge Slat Position Indicating System > AMBER LE LIGHT ON WITH FLAPS SET TO 15 DEGREES. NR 6 LE SLAT DOES NOT INDICATE EXTEND. REPLACED NR 6 SLAT POSITION INDICATING SWITCH. OPS CHECKS GOOD IAW MM CHAPTER 27-82-11.(STATUS:SUPP/CLOSED). - [SDR XN0A1263](https://openairdocs.org/sdr/XN0A1263.md): Cabin Pressure · malfunctioned · Sep 13, 2005 · N76752 · Boeing 727227 · Cabin Pressure Control System > AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE - AUTO, STANDBY OR MANUAL AC OR DC. TRANSFERRED TO MEL 5718 IAW MEL 21-16-2D. PLACARDS INSTALLED CAT-C. - [SDR XN0A1254](https://openairdocs.org/sdr/XN0A1254.md): Brake Assy · vibrates · Aug 10, 2005 · N76752 · Boeing 727227 · Brake Anti-Skid Section > ON TAXIOUT, BRAKES VIBRATE WHEN APPLIED. BLED BRAKES AS REQ'D IAW B727 MM REF 32-41-0, SYSTEM OPS CHECKS GOOD. - [SDR XN0A1253](https://openairdocs.org/sdr/XN0A1253.md): Exciter · failed · Aug 9, 2005 · N76752 · Boeing 727227 · Exciter > ON ENGINE START NR 2 ENGINE WOULD NOT START, START VALVE OPENS PRESSURE DROP NO EGT. REMOVED AND REPLACED NR 2 ENG EXCITER BOX IAW MM 74-11-1, OPS GOOD. - [SDR XN0A1236](https://openairdocs.org/sdr/XN0A1236.md): Warning Light · illuminated · May 13, 2005 · N76752 · Boeing 727227 · Pneumatic System > DURING EMERGENCY DESCENT, LT DUCT OVERHEAT LIGHT TRIP, PERFORMED ALL CHECKLIST. - [SDR XN0A1235](https://openairdocs.org/sdr/XN0A1235.md): Ignition Unit · malfunctioned · May 11, 2005 · N76752 · Boeing 727227 · Ignition System > NR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD. - [SDR XNOA1225](https://openairdocs.org/sdr/XNOA1225.md): Engine · inoperative · May 11, 2005 · N76752 · Boeing 727227 · Ignition System > NR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD. - [SDR XNOA1231](https://openairdocs.org/sdr/XNOA1231.md): Selector Switch · burned out · Apr 14, 2005 · N76752 · Boeing 727227 · Indicating/Recording System > AFTER STARTING NR 3 ENGINE, AC FREQUENCY METER PEGGED OUT AND SMOKE POURED OUT OF FREQ (AC) SELECTOR SWITCH. REMOVED AND REPLACED AC FREQ METER SELECTOR SWITCH AND OPS CHECK OKAY IAW B727 MM 24-20-00. - [SDR XN0A1227](https://openairdocs.org/sdr/XN0A1227.md): Warning Light · illuminated · Dec 24, 2004 · N76752 · Boeing 727227 · Antenna/Radome Anti-Ice/De-Ice System > NR 3 ENGINE CSD LOW PRESSURE WARNING LIGHT ON WITH NO FREG. DISCONNECTED NR 3 CSD DEFERRED NR 3 GENERATOR INOP IAW ENA B727 MEL 24-1 PROCEDURES DMI 4858 CAT-B ITEM. PLACARDS INSTALLED. - [SDR XNOA1183](https://openairdocs.org/sdr/XNOA1183.md): Switch · out of adjust · Apr 13, 2004 · N76752 · Boeing 727227 · Door Warning System > DURING CLIMB, MAIN CARGO DOOR LIGHT ILLUMINATED. ADJUSTED DOOR CLOSED SWITCH IAW HAMILTON-TIMCO SUPPLEMENTAL MM 7-11-1. OPS CHECKS GOOD IAW HAMILTON TIMCO-SUPPLEMENTAL MM 4.1.1 - [SDR XNOA1179](https://openairdocs.org/sdr/XNOA1179.md): Engine · malfunctioned · Mar 5, 2004 · N76752 · Boeing 727227 · Engine (Turbine/Turboprop) > NR 2 ENGINE WILL NOT ACHIEVE TAKE-OFF POWER. PERFORMED NR 2 ENGINE RUN. NR 2 ENGINE MAKES ITS TARGET POWER IAW P&W JT8D MM 72-00-00. NO DEFECTS NOTED. (STATUS: ORIG/CLOSED) - [SDR CALA9801670](https://openairdocs.org/sdr/CALA9801670.md): Hyd Line · leaking · Sep 9, 1998 · N76752 · Boeing 727227 · Hydraulic System, Main > THE A HYDRAULIC SYSTEM WAS LOST ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE A SYSTEM HYDRAULIC PRESSURE LINE IN AFT AIRSTAIRS TO FIREWALL LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMOVED AND REPLACED. T - [SDR CALA9800736](https://openairdocs.org/sdr/CALA9800736.md): Hyd Line · leaking · May 3, 1998 · N76752 · Boeing 727227 · Hydraulic System, Main > LOSS OF A-SYSTEM HYDRAULIC FLUID UPON RETRACTING THE LANDING GEAR. REMOVED AND REPLACED TAIL SKID RIGHT HYDRAULIC LINE PER MM 32-71-12. - [SDR CALA9800138](https://openairdocs.org/sdr/CALA9800138.md): Bulkhead · cracked · Jan 29, 1998 · N76752 · Boeing 727227 · Fuselage Main, Bulkhead > INSPECTION FOUND, A 1 CRACK IN FORWARD FACE OF STA 1183 BULKHEAD ON RT SIDE ABOVE OUTFLOW VALVE. A WEB REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C31446, SRM 51-30-0, AND ECRA 553A0022. - [SDR CALA9800129](https://openairdocs.org/sdr/CALA9800129.md): Battery Pack · discharged · Jan 27, 1998 · N76752 · Boeing 727227 · Emergency Lighting > INSPECTION FOUND, THE AFT ENTRY EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. - [SDR CALA9800128](https://openairdocs.org/sdr/CALA9800128.md): Rib · cracked · Jan 27, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A 2 INCH CRACK AT FASTENER OF RT WING LEADING EDGE RIB, INBOARD OF NR 4 LEADING EDGE FLAP, AT L/E STA 130. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. - [SDR CALA9800127](https://openairdocs.org/sdr/CALA9800127.md): Skin · cracked · Jan 27, 1998 · N76752 · Boeing 727227 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND A.5, 1, AND 2 CRACK IN RT SIDE OF VERTICAL STABILIZER SKIN LOWER SECTION AT STA 1343. THE AREA WAS REPAIRED IAW ECRA 5530-01190. - [SDR CALA9800126](https://openairdocs.org/sdr/CALA9800126.md): Stop · cracked · Jan 27, 1998 · N76752 · Boeing 727227 · Passenger/Crew Doors > INSPECTION FOUND A 1 CRACK IN L-1 AFT UPPER DOOR STOP AT FITTING. THE L-1 AFT UPPER DOOR STOP WAS REMOVED AND REPLACED IAW SRM 52-40-1. - [SDR CALA9800105](https://openairdocs.org/sdr/CALA9800105.md): Rib · cracked · Jan 24, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A 2 INCH CRACK AT FASTENER IN RT WING RIB INBOARD OF NR 4 LEADING EDGE FLAP AT L/E STA 130. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. - [SDR CALA9800078](https://openairdocs.org/sdr/CALA9800078.md): Bracket · cracked · Jan 16, 1998 · N76752 · Boeing 727227 · Wing Miscellaneous Structure > INSPECTION FOUND A.2812 INCH CRACK OUTBOARD OF NR 8 SPOILER ACTUATOR IN RT WING INBOARD TRAILING EDGE PANEL SUPPORT BRACKET AT WS 232. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5750-0287 - [SDR CALA9800077](https://openairdocs.org/sdr/CALA9800077.md): Skin · cracked · Jan 16, 1998 · N76752 · Boeing 727227 · Wing, Plate/Skin > INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE LOWER SKIN ABOVE NR 5 LEADING EDGE FLAP ACTUATOR, WS 224. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. - [SDR CALA9800076](https://openairdocs.org/sdr/CALA9800076.md): Angle · cracked · Jan 16, 1998 · N76752 · Boeing 727227 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT, RT SIDE, STA 1283. THE ANGLE WAS REMOVED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. - [SDR CALA9800075](https://openairdocs.org/sdr/CALA9800075.md): Light · inoperative · Jan 15, 1998 · N76752 · Boeing 727227 · Emergency Lighting > INSPECTION FOUND EMERGENCY FLOOD LIGHT AT LEFT SIDE OVER AFT AIRSTAIRS INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED. - [SDR CALA9800073](https://openairdocs.org/sdr/CALA9800073.md): Rib · cracked · Jan 15, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF NR 6 LEADING EDGE SLAT STA 234. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9800072](https://openairdocs.org/sdr/CALA9800072.md): Rib · cracked · Jan 15, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A.75 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN ABOVE PNEUMATIC DUCT FORWARD SUPPORT BRACKET AT FSS 106.8. A REPAIR WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9800071](https://openairdocs.org/sdr/CALA9800071.md): Skin · cracked · Jan 15, 1998 · N76752 · Boeing 727227 · Wing, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD HOOK. THE CRACK WAS STOP DRILLED PER SRM 51-10-1, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4. - [SDR CALA9800070](https://openairdocs.org/sdr/CALA9800070.md): Skin · bent · Jan 15, 1998 · N76752 · Boeing 727227 · Aileron Tabs > INSPECTION FOUND LT WING OUTBOARD AILERON TAB LOWER LEADING EDGE SKIN BENT AND DEBONDED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41. - [SDR CALA9800067](https://openairdocs.org/sdr/CALA9800067.md): Stringer · cracked · Jan 15, 1998 · N76752 · Boeing 727227 · Vertical Stabilizer > INSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER STRINGER NR 9 BETWEEN RIB NR 7 AND NR 8. THE CRACK WAS LOCATED AT ATTACH BOLT. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2. - [SDR CALA9800066](https://openairdocs.org/sdr/CALA9800066.md): Stringer · cracked · Jan 15, 1998 · N76752 · Boeing 727227 · Vertical Stabilizer > INSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER STRINGER NR 8 BETWEEN RIB NR 8 AND NR 9. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2. - [SDR CALA9800064](https://openairdocs.org/sdr/CALA9800064.md): Stringer · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Longeron/Stringer > INSPECTION FOUND A.5 INCH CRACK AT FASTENER HOLE IN LT WING SECOND UPPER STRINGER FROM REAR SPAR ABOVE RIB AT WS 629. THE FASTENERS AND CLAMPS WERE REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW EA 5762-01 - [SDR CALA9800063](https://openairdocs.org/sdr/CALA9800063.md): Stringer · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Longeron/Stringer > INSPECTION FOUND A.75 INCH CRACK IN RT WING STRINGER AT WS 656.5, TOP OF RIB ATTACH POINT ACCESS THROUGH PANEL 7617. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050. - [SDR CALA9800062](https://openairdocs.org/sdr/CALA9800062.md): Rib · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN LOWER EDGE AT FSS 106.8. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9800061](https://openairdocs.org/sdr/CALA9800061.md): Rib · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2. - [SDR CALA9800060](https://openairdocs.org/sdr/CALA9800060.md): Skin · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Plate/Skin > INSPECTION FOUND FOUR.5 INCH CRACKS AROUND FASTENERS OUTBOARD OF LAMP LIGHT IN WING LEADING EDGE INTERNAL SKIN AT FSS 106. THE CRACKED AREAS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-6. - [SDR CALA9800059](https://openairdocs.org/sdr/CALA9800059.md): Rib · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Rib/Bulkhead > INSPECTION FOUND A.5 INCH CRACK INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STA 130 ABOVE HOT AIR DUCT PLENUM. ALSO, A.5 INCH CRACK WAS FOUND INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STATION 130 BELOW LIGHTENING HOLE AREA. DOUBLER REPAIRS WERE F - [SDR CALA9800058](https://openairdocs.org/sdr/CALA9800058.md): Skin · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Plate/Skin > INSPECTION FOUND A 2 INCH CRACK IN LEADING EDGE SKIN AT DOUBLER STRAP INSIDE LT WING DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR AT WS 224. THE CRACKED DOUBLER WAS REMOVED, A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. - [SDR CALA9800057](https://openairdocs.org/sdr/CALA9800057.md): Stringer · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Longeron/Stringer > INSPECTION FOUND A.5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50. THE FASTENERS AND CLAMPS WERE REMOVED. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050. - [SDR CALA9800056](https://openairdocs.org/sdr/CALA9800056.md): Skin · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 4 SLAT OUTBOARD HOOK ATTACHES. A DOUBLER WAS INSTALLED IAW SRM 57-30-4. - [SDR CALA9800055](https://openairdocs.org/sdr/CALA9800055.md): Skin · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Wing, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 3 SLAT INBOARD HOOK ATTACHES. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4. - [SDR CALA9800054](https://openairdocs.org/sdr/CALA9800054.md): Skin · corroded · Jan 14, 1998 · N76752 · Boeing 727227 · Trailing Edge Flaps > INSPECTION FOUND LT WING INBOARD MIDFLAP SKIN CORRODED OUTBOARD OF INBOARD CARRIAGE MOUNT AREA. A SKIN REPAIR WAS INSTALLED IAW SRM 57-50-4. - [SDR CALA9800053](https://openairdocs.org/sdr/CALA9800053.md): Brackets · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Leading Edge Slat Actuator > INSPECTION FOUND A.5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1. - [SDR CALA9800052](https://openairdocs.org/sdr/CALA9800052.md): Brackets · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Leading Edge Slat Actuator > INSPECTION FOUND A.5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-1. - [SDR CALA9800051](https://openairdocs.org/sdr/CALA9800051.md): Gusset · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Vertical Stabilizer > INSPECTION FOUND A.5 INCH CRACK AT TOP CORNER AND A.5 INCH CRACK AT LOWER CORNER OF GUSSET ON RT SIDE OF VERTICAL STABILIZER AT STRINGER 9 BETWEEN RIB NR 6 AND NR 7. THE GUSSET PLATE WAS REMOVED, A NEW GUSSET PLATE WAS FABRICATED AND INSTALLED IAW SRM 55-30 - [SDR CALA9800050](https://openairdocs.org/sdr/CALA9800050.md): Support · corroded · Jan 14, 1998 · N76752 · Boeing 727227 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 996, RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6. - [SDR CALA9800049](https://openairdocs.org/sdr/CALA9800049.md): Stringer · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A.5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5. - [SDR CALA9800048](https://openairdocs.org/sdr/CALA9800048.md): Stringer · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A.5 INCH CRACK IN END OF STRINGER 15L AT STA 720C. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5. - [SDR CALA9800047](https://openairdocs.org/sdr/CALA9800047.md): Doubler · cracked · Jan 14, 1998 · N76752 · Boeing 727227 · Fuselage Miscellaneous Structure > INSPECTION FOUND THREE CRACKS AT HI-LOKS ON DOUBLER UPPER SIDE OF CARGO DOOR FRAME CUTOUT BETWEEN FS 604 TO 608, STRINGER 10R. THE CRACKS WERE.25 TO 1 INCH LONG. THE FASTENERS AND DOUBLER WERE REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51- Next page: https://openairdocs.org/deregistered/N76752-2006-09-25/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N76752' AND deregistration_id = 'N76752-2006-09-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N76752-2006-09-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.